The present disclosure relates to a water tank configured for operation in an aircraft (50). The tank comprises a rigid tank shell (110), and a pressure compensation mechanism (120) configured to equalise a pressure inside of the rigid tank shell with an environment. The pressure compensation mechanism comprises a shutoff member (122) configured to move between a closed position, a first open position allowing air to enter the rigid tank shell and a second open position allowing air to leave the rigid tank shell.


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    Title :

    PRESSURELESS WATER TANK FOR OPERATION IN AN AIRCRAFT, AIRCRAFT SECTION AND AIRCRAFT HAVING A WATER TANK


    Additional title:

    DRUCKLOSER WASSERTANK FÜR DEN BETRIEB IN EINEM FLUGZEUG, FLUGZEUGABSCHNITT UND FLUGZEUG MIT WASSERTANK
    RÉSERVOIR D'EAU SANS PRESSION POUR FONCTIONNEMENT DANS UN AÉRONEF, SECTION D'AÉRONEF ET AÉRONEF COMPORTANT UN RÉSERVOIR D'EAU


    Contributors:

    Publication date :

    2024-03-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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